WO2017073417A1 - 熱式流量計 - Google Patents

熱式流量計 Download PDF

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Publication number
WO2017073417A1
WO2017073417A1 PCT/JP2016/080893 JP2016080893W WO2017073417A1 WO 2017073417 A1 WO2017073417 A1 WO 2017073417A1 JP 2016080893 W JP2016080893 W JP 2016080893W WO 2017073417 A1 WO2017073417 A1 WO 2017073417A1
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WO
WIPO (PCT)
Prior art keywords
passage
sub
flow meter
discharge port
thermal flow
Prior art date
Application number
PCT/JP2016/080893
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English (en)
French (fr)
Japanese (ja)
Inventor
征史 深谷
忍 田代
暁 上ノ段
斉藤　友明
直生 斎藤
Original Assignee
日立オートモティブシステムズ株式会社
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by 日立オートモティブシステムズ株式会社 filed Critical 日立オートモティブシステムズ株式会社
Priority to DE112016004950.1T priority Critical patent/DE112016004950T5/de
Priority to US15/771,007 priority patent/US10670439B2/en
Priority to CN201680058323.3A priority patent/CN108139248B/zh
Publication of WO2017073417A1 publication Critical patent/WO2017073417A1/ja

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    • G—PHYSICS
    • G01—MEASURING; TESTING
    • G01F—MEASURING VOLUME, VOLUME FLOW, MASS FLOW OR LIQUID LEVEL; METERING BY VOLUME
    • G01F1/00—Measuring the volume flow or mass flow of fluid or fluent solid material wherein the fluid passes through a meter in a continuous flow
    • G01F1/68—Measuring the volume flow or mass flow of fluid or fluent solid material wherein the fluid passes through a meter in a continuous flow by using thermal effects
    • G01F1/684—Structural arrangements; Mounting of elements, e.g. in relation to fluid flow
    • G01F1/6842—Structural arrangements; Mounting of elements, e.g. in relation to fluid flow with means for influencing the fluid flow
    • G—PHYSICS
    • G01—MEASURING; TESTING
    • G01F—MEASURING VOLUME, VOLUME FLOW, MASS FLOW OR LIQUID LEVEL; METERING BY VOLUME
    • G01F5/00—Measuring a proportion of the volume flow

Definitions

  • the present invention relates to a thermal flow meter for measuring the flow rate of a gas such as air.
  • a thermal flow meter that measures the flow rate of a gas such as air is equipped with a flow rate detection unit for measuring the flow rate, and heat transfer is performed between the flow rate detection unit and the gas to be measured, thereby reducing the flow rate of the gas. It is configured to measure.
  • the flow rate measured by the thermal flow meter is widely used as an important control parameter for various devices.
  • a feature of the thermal flow meter is that it can measure a gas flow rate, for example, a mass flow rate, with relatively high accuracy compared to other types of flow meters.
  • this thermal flow meter it is desired to further improve the measurement accuracy of the gas flow rate.
  • a vehicle equipped with an internal combustion engine has a very high demand for fuel saving and exhaust gas purification.
  • a thermal flow meter that measures the amount of intake air that is guided to an internal combustion engine includes a sub-passage that takes in a portion of the intake air amount, and a flow rate detection unit that is disposed in the sub-passage. By performing heat transfer between them, the flow rate of the air flowing through the auxiliary passage is measured, and an electric signal representing the amount of intake air guided to the internal combustion engine is output.
  • the sub-passage has a structure in which the flow that flows from the inlet is branched toward the bypass outlet and the dust discharge port, and the dust that flows from the inlet is discharged from the dust discharge port. This prevents the dust from colliding with the flow rate detection unit and damaging the flow rate detection unit.
  • Patent Document 1 Japanese Patent Application Laid-Open No. 2012-202755 (Patent Document 1), as shown in paragraph 0023 and FIG.
  • An intake outlet that opens toward the downstream side of the intake mainstream with respect to the intake path, a straight line that extends linearly from the inlet, and that goes straight in the same direction as the main intake flow in the intake path, and that goes straight on the straight path
  • a circuit that circulates the intake air and directs it toward the outlet.
  • a dust discharge path for discharging dust is linearly connected to the straight path, and the downstream end of the dust discharge path is a dust discharge port that opens toward the downstream side of the intake mainstream with respect to the intake path.
  • the air flow rate measuring device is a sub-branch that is branched in the middle of the bypass flow path.
  • a flow sensor is arranged in the bypass flow path.
  • vertical to the opening surface of a bypass exit is provided so that it may go to the direction away from a branch. That is, the opening surface does not face straight in the mainstream downstream direction, but is formed to face a direction inclined downward in the height direction with respect to the mainstream downstream direction.
  • downstream end of the second wall surface Since the downstream end of the second wall surface is located upstream of the downstream end of the third wall surface, it is less likely that dust that collides with the third wall surface and bounces back will collide with the second wall surface.
  • the dust colliding with the third wall surface is also easily discharged from the bypass outlet. For this reason, it is possible to prevent dust from reaching the flow sensor.
  • both Patent Documents 1 and 2 include the center of gravity of the opening surface where the dust discharge port and the bypass outlet open to the main passage, and on the basis of a plane perpendicular to the opening surface and parallel to the insertion direction of the thermal flow meter, Since the thickness of the thermal flow meter in the direction orthogonal to the direction of insertion of the thermal flow meter and the flow direction in the intake pipe is provided symmetrically, in the condition where the main intake air flows forward from the upstream side to the downstream side, the thermal type A pair of wake vortices generated on the lower end surface side of the measurement unit main body of the flowmeter are also almost symmetrical.
  • An object of the present invention is to provide a thermal flow meter that suppresses at least a flow flowing out from a dust discharge port from being hindered by a backflow generated by a wake vortex on the lower end surface side of the measurement flow unit main body of the thermal flow meter.
  • the feature of the present invention is that at least the opening of the dust discharge port is shifted from the reverse flow direction with respect to the reverse flow formed by the wake vortex generated at the lower end surface of the measurement unit main body in which the dust discharge port is formed. It is characterized by being.
  • the air flow flowing out from the dust discharge port is caused by the reverse flow generated by the downstream vortex on the downstream side of the measurement unit main body and the front surface.
  • FIG. 2A It is an internal combustion engine control system figure using the thermal type flow meter concerning the present invention. It is a front view which shows the external appearance of the thermal type flow meter which becomes the 1st Embodiment of this invention. It is a left view of the thermal type flow meter shown in Drawing 2A. It is a rear view of the thermal type flow meter shown in FIG. 2A. It is a right view of the thermal type flow meter shown in FIG. 2A. It is a front view which shows the structure in the housing which removed the table
  • FIG. 2B is a schematic conceptual diagram of a BB cross section of FIG. 2D. It is the schematic diagram which showed the channel
  • FIG. 12 It is the schematic diagram which looked at the thermal type flow meter shown in FIG. 12 from the left side. It is EE sectional drawing of FIG. It is the schematic diagram which showed the channel
  • FIG. 16 is a sectional view taken along line FF in FIG. 15. It is the schematic diagram which showed the channel
  • FIG. 18 is a sectional view taken along line GG in FIG.
  • FIG. 1 shows the configuration of an electronic fuel injection type internal combustion engine control system.
  • intake air is sucked from the air cleaner 122 as a gas to be measured IA, and an intake pipe 71 that is a pipe line in which a main passage 124 is formed.
  • intake body a throttle body 126, and an intake manifold 128.
  • the flow rate of the gas to be measured IA that is the intake air led to the combustion chamber is measured by the thermal flow meter 30, and fuel is supplied from the fuel injection valve 152 based on the measured flow rate, and the gas to be measured that is the intake air. Together with IA, it is introduced to the combustion chamber in the form of an air-fuel mixture.
  • the fuel injection valve 152 is provided at the intake port of the internal combustion engine, and the fuel injected into the intake port forms an air-fuel mixture together with the measured gas IA that is intake air, and is connected via the intake valve 116. It is guided to the combustion chamber and burns to generate mechanical energy.
  • the thermal flow meter 30 can be used not only for the method of injecting fuel into the intake port of the internal combustion engine shown in FIG. 1 but also for the method of directly injecting fuel into each combustion chamber. In both types, the basic concept of the control parameter measurement method including the method of using the thermal flow meter 30 and the control method of the internal combustion engine including the fuel supply amount and ignition timing is substantially the same. A method of injecting fuel into the port is shown in FIG.
  • the fuel and air guided to the combustion chamber form a mixed state of fuel and air, and are ignited explosively by spark ignition of the spark plug 154 to generate mechanical energy.
  • the combusted gas is led from the exhaust valve 118 to the exhaust pipe, and is exhausted from the exhaust pipe as exhaust EA.
  • the flow rate of the gas to be measured IA that is the intake air led to the combustion chamber is controlled by a throttle valve 132 whose opening degree changes based on the operation of the accelerator pedal.
  • the fuel supply amount is controlled based on the flow rate of the intake air guided to the combustion chamber, and the driver controls the flow rate of the intake air guided to the combustion chamber by controlling the opening degree of the throttle valve 132 so that the internal combustion engine is controlled.
  • the generated mechanical energy can be controlled.
  • the flow rate, humidity, and temperature of the measurement target gas IA that is the intake air that is taken in from the air cleaner 122 and flows through the main passage 124 are measured by the thermal flow meter 30, and the flow rate, humidity, and temperature of the intake air are measured from the thermal flow meter 30.
  • the electric signal to be represented is input to the control device 200.
  • the output of the throttle angle sensor 144 that measures the opening degree of the throttle valve 132 is input to the control device 200, and the positions and states of the piston 114, the intake valve 116, and the exhaust valve 118 of the internal combustion engine, and the rotational speed of the internal combustion engine. Is measured, the output of the rotation angle sensor 146 is input to the control device 200.
  • the output of the oxygen sensor 148 is input to the control device 200.
  • the control device 200 calculates the fuel injection amount and the ignition timing based on the flow rate, humidity, and temperature of the intake air that is the output of the thermal flow meter 30 and the rotational speed of the internal combustion engine from the rotation angle sensor 146. Based on these calculation results, the amount of fuel supplied from the fuel injection valve 152 and the ignition timing ignited by the spark plug 154 are controlled. The fuel supply amount and ignition timing are actually based on the intake air temperature and throttle angle change state measured by the thermal flow meter 30, the engine speed change state, and the air-fuel ratio state measured by the oxygen sensor 148. Are controlled. The control device 200 further controls the amount of air that bypasses the throttle valve 132 by the idle air control valve 156 in the idle operation state of the internal combustion engine, thereby controlling the rotational speed of the internal combustion engine in the idle operation state.
  • the fuel supply amount and ignition timing which are the main control amounts of the internal combustion engine, are all calculated using the output of the thermal flow meter 30 as a main parameter. Therefore, improvement in measurement accuracy of the thermal flow meter 30, suppression of changes over time, and improvement in reliability are important in terms of improving the control accuracy of the vehicle and ensuring reliability.
  • improvement in measurement accuracy of the thermal flow meter 30, suppression of changes over time, and improvement in reliability are important in terms of improving the control accuracy of the vehicle and ensuring reliability.
  • the dust discharge port and the bypass outlet include the center of gravity of the opening surface that opens in the main passage, and a plane perpendicular to the opening surface and parallel to the insertion direction of the thermal flow meter is formed.
  • the thickness of the thermal flow meter in the direction orthogonal to the insertion direction of the thermal flow meter and the flow direction in the intake pipe is provided symmetrically (substantially the same length), so the main intake air flows from the upstream side to the downstream side. Under the condition of forward flow, the pair of wake vortices generated on the downstream side of the thermal flow meter is also almost symmetrical.
  • the present invention proposes a thermal flow meter configured to suppress at least the air flow flowing out from the dust discharge port from being obstructed by the backflow generated by the wake vortex at the lower end surface of the measurement unit main body.
  • FIG. 2A to 2D show the appearance of the thermal type flow meter 30 according to the first embodiment of the present invention.
  • 2A is a front view of the thermal flow meter 30
  • FIG. 2B is a left side view
  • FIG. 2C is a rear view
  • FIG. 2D is a right side view.
  • the thermal flow meter 30 includes a housing 302, a front cover 303, and a back cover 304.
  • the housing 302 has an external connection portion (connector portion) having a flange 312 for fixing the thermal flow meter 30 to the intake body constituting the main passage and an external terminal for electrical connection with an external device.
  • 305 and a measurement unit main body 310 for measuring the air flow rate.
  • a sub-passage groove for making a sub-passage is provided inside the measurement unit main body 310.
  • the measurement unit main body 310 includes a housing 302, a front cover 303, and a back cover 304. By covering the housing 302 with the front cover 303 and the back cover 304, a casing having a sub-passage is formed.
  • the measurement unit main body 310 includes a flow rate detection unit 602 for measuring the flow rate of the measurement target gas IA flowing through the main passage and a temperature detection unit 452 for measuring the temperature of the measurement target gas IA flowing through the main passage.
  • a circuit package 400 is provided (see FIGS. 3A and 3B).
  • the measuring unit main body 310 is supported in a cantilever manner in the main passage by fixing the flange 312 to an intake pipe (intake passage) 71 which is a pipe line.
  • intake pipe 71 is indicated by a virtual line. Therefore, the thermal flow meter 30 is fixed by inserting the measurement unit main body 310 in a direction orthogonal to the main passage 124.
  • the measuring section main body 310 of the thermal flow meter 30 has a shape extending long from the flange 312 toward the center of the main passage 124 in the radial direction, and a gas to be measured such as intake air at the tip on the upper end surface side.
  • a main intake port 350 (see FIG. 2B) for taking a part of IA into the sub-passage is provided, and a bypass outlet 352 (see FIG. 2D) for returning the measured gas IA from the sub-passage to the main passage 124. It is provided on the lower end surface of the measurement unit main body 310.
  • the main intake port 350 is formed in the upper end surface (the side into which the measurement target gas IA flows) of the measurement unit main body 310 of the thermal flow meter 30.
  • the gas at a portion away from the inner wall surface of the main passage 124 can be taken into the sub-passage. it can. Thereby, it becomes difficult to be influenced by the temperature of the inner wall surface of the main passage, and a decrease in measurement accuracy of the gas flow rate and temperature can be suppressed.
  • the main intake port 350 is provided at the distal end portion of the thin and long measuring unit 310 extending from the flange 312 toward the center of the main passage. Gas can be taken into the sub-passage (measurement passage).
  • the dust discharge port 355 of the sub passage is also provided on the lower end surface side of the distal end portion of the measurement unit main body 310, the gas flowing in the sub passage can be returned to the vicinity of the center portion of the main passage 124 having a high flow velocity. it can.
  • the measuring unit main body 310 has a shape that extends long along the axis from the outer wall of the main passage 124 toward the center.
  • the width of the measuring unit main body 310 (the length in the air flow direction) is shown in FIGS. 2B and 2D. As described in the above, it has a narrow shape. That is, the measurement unit main body 310 of the thermal flow meter 30 has a thin side surface and a substantially rectangular front surface.
  • the thermal flow meter 30 can be provided with a sufficiently long sub-passage with a reduced fluid resistance with respect to the gas to be measured IA.
  • the housing 302 has an upper end surface and a lower end surface along the flow of air flowing through the intake pipe 71. As shown in FIGS. 2B and 2D, the main intake port 350 is opened at the upper end surface, and the lower end surface has The dust outlet 355 and the bypass outlet 352 are opened.
  • the temperature detector 452 for measuring the temperature of the gas IA to be measured is located at the center of the measuring unit main body 310, and the upstream outer wall in the measuring unit main body 310 is recessed toward the downstream side from the upstream outer wall. A shape protruding toward the upstream side is provided.
  • the front cover 303 and the back cover 304 are formed in a thin plate shape and have a shape with a wide cooling surface. For this reason, the thermal flow meter 30 has an effect that air resistance is reduced, and further, the thermal flow meter 30 is easily cooled by the gas to be measured flowing through the main passage 124.
  • the external terminal includes a terminal for outputting a flow rate and temperature as measurement results, and a power supply terminal for supplying DC power.
  • the correction terminal is a terminal used to store a correction value related to the thermal flow meter 30 in a memory inside the thermal flow meter 30.
  • FIG. 3A and 3B show the internal structure of the housing 302 with the front cover 303 or the back cover 304 removed from the thermal flow meter 30.
  • FIG. 3A is a front view showing the internal configuration of the housing 302 with the front cover 303 removed from the thermal flow meter 30, and
  • FIG. 3B shows the internal configuration of the housing 302 with the back cover 304 removed from the thermal flow meter 30.
  • the housing 302 is provided with a sub-passage groove for forming a sub-passage on the distal end side of the measurement unit main body 310.
  • the sub passage is a passage formed in the thermal flow meter 30 in order to take in a part of the gas to be measured flowing through the main passage 124.
  • auxiliary passage grooves 331 and 332 are provided on both the front and back surfaces of the housing 302.
  • both the back side sub-passage groove 331 and the front side sub-passage groove 332 are formed in the housing 302 by using dies provided on both sides of the housing 302 when the housing 302 is molded (resin molding process).
  • a through portion 382 that penetrates the housing 302 is formed so as to connect them, and the flow rate detecting element (flow rate detecting portion) 602 of the circuit package 400 can be disposed in the through portion 382.
  • a part of the measurement target gas IA flowing through the main passage is taken into the back side sub-passage groove 331 from the main intake port 350 via the inlet groove 351 and flows through the back side sub-passage groove 331.
  • the back cover 304 By covering the back cover 304 with the back side sub-passage groove 331, a part of the upstream side of the first passage 31 and the second passage 32 of the sub-passage is formed in the thermal flow meter 30.
  • the first passage 31 inertias the pollutant formed from the main intake port 350 for taking in the measurement target gas IA flowing through the main passage 124 to the dust discharge port 355 for discharging a part of the taken measurement target gas IA.
  • This is a discharge passage to be separated.
  • the second passage 32 is a flow rate measurement passage formed toward the flow rate detection unit 602 from the sub intake port 34 for taking in the measurement target gas IA flowing in the first passage 31.
  • the main intake port 350 is opened to face the upstream side of the main passage 124 on the upper end surface side of the measurement unit main body 310, and the dust discharge port 355 is formed on the lower end surface side of the measurement unit main body 310. Opening facing the downstream side, the opening area of the dust discharge port 355 is smaller than the opening area of the main intake port 350. As a result, the gas IA to be measured from the main intake port 350 can easily flow into the second passage 32.
  • the passage groove of the second passage 32 (passage to the flow rate detection unit 602) has a shape that becomes deeper as it advances in the flow direction, and in the front side direction as it flows along the groove.
  • the gas to be measured IA moves gradually.
  • the back side sub-passage groove 334 is provided with a steeply inclined portion 347 that suddenly deepens in the upstream portion 342 of the circuit package 400. A part of the air having a small mass moves along the steeply inclined portion 347 and flows toward the measurement channel surface 430 in the upstream portion 342 of the through portion 382 of the circuit package 400 as shown in FIG.
  • a foreign substance having a large mass cannot easily flow along the steeply inclined portion 347 because it is difficult to change the course due to centrifugal force, and flows along the measurement channel back surface 431 shown in FIG. After that, it passes through the downstream portion 341 of the penetrating portion 382 and flows through the front side auxiliary passage groove 332 shown in FIG. 3A.
  • the portion of the circuit package 400 that includes the measurement flow path surface 430 is disposed in the cavity of the through portion 382, and the through portion 382 is provided on the left and right sides of the circuit package 400 having the measurement flow passage surface 430.
  • the groove 334 and the front side auxiliary passage groove 332 are connected.
  • this flow rate measurement principle may be a general detection principle for a thermal flow meter, and flows through the main passage based on the measurement value measured by the flow rate detection unit 602 of the circuit package 400 as in this embodiment. As long as the flow rate of the gas to be measured can be detected, the configuration for detection is not particularly limited.
  • An outlet groove 353 forming an outlet 352 is discharged into the main passage 124.
  • the second passage formed by the back side sub-passage groove 334 is curved toward the flange direction from the tip of the housing 302 while drawing a curve, and the measured gas IA flowing through the sub-passage is closest to the flange side.
  • the flow is in the opposite direction to the flow of the main passage 124.
  • the sensor upstream side passage 32a provided on the back surface side of the second passage 32 provided on one side of the housing 302 is a second portion provided on the other side of the second passage 32 provided on the one side of the housing 302.
  • the sensor downstream side passage 32b provided on the surface side of the second passage 32 is connected.
  • the front end side of the circuit package 400 is disposed in the cavity of the through portion 382.
  • the space of the upstream portion 342 located on the upstream side of the circuit package 400 and the space of the downstream portion 341 located on the downstream side of the circuit package 400 are included in the penetration portion 382, and the penetration portion 382 is as described above.
  • the housing 302 is pierced so as to penetrate the front surface side and the back surface side.
  • the downstream upstream side passage formed by the sensor upstream side passage 32 a formed by the front side secondary passage groove 334 on the front surface side of the housing 302 and the back side secondary passage groove 332 on the back surface side. 32b communicates.
  • the space on the measurement flow path surface 430 side and the space on the measurement flow path back surface 431 side are divided by the circuit package 400 inserted in the housing 302, and depending on the housing 302 It has not been.
  • One space formed by the space of the upstream portion 342, the space of the downstream portion 341, the space on the measurement flow channel surface 430 side, and the space on the measurement flow channel back surface 431 side is the front and back surfaces of the housing 302.
  • the circuit package 400 inserted into the housing 302 protrudes in a cantilever manner in this one space.
  • the sub-passage grooves can be formed on both surfaces of the housing 302 in a single resin molding step, and the structure connecting the sub-passage grooves on both surfaces can be formed together.
  • the circuit package 400 is fixed by being embedded in resin fixing parts 372, 373, and 376 of the housing 302.
  • Such a fixing structure can be mounted on the thermal flow meter 30 by insert molding the circuit package 400 into the housing 302 simultaneously with resin molding of the housing 302.
  • the back side sub-passage groove 334 includes a first passage wall 395, a back side sub-passage inner peripheral wall (second passage wall) 392, and a back side sub-passage outer peripheral wall ( Second wall 391).
  • the front end portions of the back side sub-passage inner peripheral wall 392 and the back side sub-passage outer peripheral wall 391 and the inner side surface of the back cover 304 are in close contact with each other, whereby the first passage 31 and the second passage of the housing 302 are in close contact with each other.
  • a sensor upstream side passage 32a of the passage 32 is formed.
  • a front side sub-passage inner peripheral wall (second passage wall) 393 and a front side sub-passage outer peripheral wall (second passage wall) 394 are provided on both sides of the front side sub-passage groove 332,
  • the downstream side sub-passage of the housing 302 is formed by the close contact between the front end of the sub-passage inner peripheral wall 393 and the sub-passage outer peripheral wall 394 and the inner side surface of the front cover 303.
  • the gas IA to be measured that has been taken in from the main inlet 350 and has flowed through the first passage 31 constituted by the back side sub-passage groove 334 flows from the right side to the left side in FIG. 3B.
  • a part of the taken measurement gas IA flows in a diverted flow into the sub intake port 34 of the second passage 32 formed to branch from the first passage 31.
  • the measured gas IA that has flowed passes through the upstream portion 342 of the penetrating portion 382 and the projection 356 provided on the surface of the measurement channel surface 430 of the circuit package 400 and the front cover 303. It flows in the direction of the flow path 386 made by
  • Other gas to be measured IA flows in the flow path 387 formed by the measurement flow path back surface 431 and the back cover 304. Thereafter, the measured gas IA that has flowed through the flow path 387 moves toward the front side sub-passage groove 332 via the downstream portion 341 of the penetrating portion 382, and merges with the measured gas IA that flows through the flow path 386.
  • the joined measurement gas IA flows through the front side sub-passage groove 332 and is discharged from the bypass outlet 352 to the main passage.
  • the sub-passage groove is such that the measured gas IA guided from the back side sub-passage groove 334 to the flow path 386 via the upstream portion 342 of the penetrating part 382 is bent more than the flow path guided to the flow path 387. Is formed. Thereby, a substance having a large mass such as dust contained in the measurement target gas IA collects in the flow path 387 with less bending.
  • the protrusion 356 forms a throttle, and the measurement gas IA is made into a laminar flow with little vortex. Further, the protrusion 356 increases the flow velocity of the measurement target gas IA. Thereby, measurement accuracy improves.
  • the protrusion 356 is formed on the front cover 303, which is a cover that faces the heat transfer surface exposed portion 436 of the flow rate detector 602 provided on the measurement flow path surface 430.
  • a hollow portion 336 is formed in the housing 302 between the flange 312 and the portion where the sub-passage groove is formed.
  • a terminal connection portion 320 that connects the connection terminal 412 of the circuit package 400 and the inner end 361 of the external terminal of the external connection portion 305 is provided.
  • the connection terminal 412 and the inner end 361 are electrically connected by spot welding or laser welding.
  • FIG. 5 is a schematic view of the BB cross section of FIG. 2D.
  • the main intake air flows forward from the upstream side to the downstream side as the gas to be measured IA, it flows from the upper side to the lower side as shown in FIG.
  • a pair of wake vortices IB are almost symmetrical with the end surfaces of the front cover 303 and the back cover 304 existing in the thickness direction. Arise.
  • These wake vortices IB merge at an intermediate position between them to form a backflow IC directed toward the lower end surface of the measurement unit main body 310 of the thermal flow meter. Since this reverse flow IC acts against the air flow flowing out from the dust discharge port 355 and the bypass outlet 352 and inhibits the outflow, the dust discharge effect is reduced and the measurement error of the mass flow rate is worsened.
  • the thickness (w1 + w2) of the main body 310 includes a center of gravity P of the opening surface where the dust discharge port 355 opens into the main passage, and is a plane (center of gravity plane perpendicular to the opening surface and parallel to the insertion direction of the thermal flow meter. (Referred to as “C”), the lengths are different (w1 ⁇ w2).
  • the center of gravity plane C is described as a reference, but in addition to this, the length W1 from the vicinity of the center of the dust discharge port 355 to the back cover 304 and the vicinity of the center of the dust discharge port 355 are shown.
  • the length W2 up to the cover 303 may have a relationship of W1 ⁇ W2.
  • the discharge direction of the air flow ID discharged from the dust discharge port 355 can be shifted with respect to the reverse flow direction of the reverse flow IC. That is, since the position of the reverse flow IC in the reverse flow direction is generated near the middle in the thickness direction between the front cover 303 and the back cover 304, if the dust discharge port 355 is opened avoiding the position near the middle, This is because it is difficult to be affected by backflow. That is, the discharge port 355 formed on the lower end surface of the measurement unit main body 310 is arranged near the front cover 303 or the back cover 304 side from the intermediate position in the thickness direction between the front cover 303 and the back cover 304. Yes.
  • the position of the opening of the dust discharge port 355 is provided at a position spaced from the center of the projection surface in the thickness direction. It is what.
  • the streamline vector of the air flow ID discharged from the discharge port 355 is opposed to the streamline vector of the backflow IC formed by the wake vortex generated at the lower end surface of the measurement unit main body 310 from the front. It is the structure which provided the discharge port 355 in the position which does not.
  • the dust discharge port 355 formed on the lower end surface of the measurement unit main body 310 of the thermal flow meter.
  • the outlet 355 includes the center of gravity P of the opening surface that opens into the main passage, and has different lengths (w1 ⁇ w2) with respect to a plane (center of gravity plane C) perpendicular to the opening surface and parallel to the insertion direction of the thermal flow meter. It is necessary to become.
  • the dust discharge port 355 may be opened at a position shifted with respect to the reverse flow direction in which the reverse flow IC travels.
  • the flow flowing out from the dust discharge port is the wake vortex on the lower end surface side of the measurement unit body of the thermal flow meter. It is possible to avoid facing the backflow caused by the front from the front, and as a result, it is possible to suppress the reduction of the dust discharge effect.
  • FIG. 6 is an enlarged view of a sub-passage portion of the housing 302 with the front cover 303 removed, and a part of the configuration is simplified or omitted.
  • the shape of the outlet groove 353 is different from that of the first embodiment. That is, the shapes of the front side sub-passage inner peripheral wall (second passage wall) 393 and the front side sub-passage outer peripheral wall (second passage wall) 394 on both sides of the front side sub-passage groove 332 are different. The position in the height direction is different.
  • FIG. 7 is an enlarged view of the right side view, and a part of the configuration is simplified or omitted.
  • the thickness (w1 + w2) of the measurement main body 310 of the thermal flow meter in the direction orthogonal to the insertion direction of the thermal flow meter at the dust discharge port position and the flow direction in the intake pipe is an opening at which the dust discharge port 355 opens into the main passage.
  • the plane includes the center of gravity P of the surface, and has different lengths (w1 ⁇ w2) on the basis of a plane perpendicular to the opening surface and parallel to the insertion direction of the thermal flow meter (center of gravity plane C). This is the same as in the first embodiment.
  • the bypass outlets 352 are arranged in parallel so as to be adjacent to the vicinity of the dust discharge outlet 355, and the opening position thereof is the length (thickness) between the front cover 303 and the back cover 304 of the measurement unit main body 310. Is located on the front cover 303 side from the middle of the direction). Therefore, the bypass outlet 352 and the dust outlet 35 are disposed at positions shifted with respect to the reverse flow direction of the reverse flow IC.
  • FIG. 8 is a cross-sectional view taken along the line CC of FIG.
  • an air flow IE flowing out from the bypass outlet 352 toward the downstream side is generated.
  • the bypass outlet 352 is also arranged at a position shifted with respect to the backflow direction of the backflow IC, the air flow IE also does not face the backflow IC from the front. For this reason, the air flow IE is hardly disturbed by the backflow IC, and the deterioration of the measurement error of the mass flow rate can be suppressed.
  • the air flow ID is not easily inhibited by the wake vortex IB, and it is possible to suppress the reduction of dust discharge effect and the deterioration of the measurement error of the mass flow rate.
  • FIG. 9 is an enlarged view of the sub-passage portion of the front view showing the state of the housing with the front cover removed, and a part of the configuration is simplified or omitted.
  • the shape of the outlet groove 353 is different from that of the second embodiment. That is, the shapes of the front side sub-passage inner peripheral wall (second passage wall) 393 and the front side sub-passage outer peripheral wall (second passage wall) 394 on both sides of the front side sub-passage groove 332 are different, and the passage toward the bypass outlet 352 It has a shape with a reduced area.
  • FIG. 10 is an enlarged view of the right side view, and a part of the configuration is simplified or omitted.
  • the thickness (w1 + w2) of the measurement main body 310 of the thermal flow meter in the direction orthogonal to the insertion direction of the thermal flow meter at the dust discharge port position and the flow direction in the intake pipe is an opening at which the dust discharge port 355 opens into the main passage.
  • the plane includes the center of gravity P of the surface, and has different lengths (w1 ⁇ w2) on the basis of a plane perpendicular to the opening surface and parallel to the insertion direction of the thermal flow meter (center of gravity plane C). This is the same as in the first embodiment.
  • the bypass outlets 352 are arranged in parallel so as to be adjacent to the vicinity of the dust discharge outlet 355, and the opening position thereof is the length (thickness) between the front cover 303 and the back cover 304 of the measurement unit main body 310. It is arranged on the front cover 303 side from the middle in the (direction). Therefore, the bypass outlet 352 and the dust outlet 35 are disposed at positions shifted with respect to the reverse flow direction of the reverse flow IC.
  • FIG. 11 is a sectional view taken along the line DD of FIG.
  • the outlet groove 353 has a shape in which the passage area is reduced toward the outlet 352, so that the strength is increased by restricting the flow.
  • the flow obtained by joining a part of the air flow IE and the air flow ID further increases the strength (dynamic pressure), and therefore the action of pushing the wake vortex IB in front of the air flow ID back to the downstream side further increases.
  • the air flow ID is less likely to be inhibited by the wake vortex IB, and it becomes easier to suppress the dust discharge effect and the deterioration of the mass flow measurement error.
  • FIG. 12 is an enlarged view of the sub-passage portion of the front view showing the state of the housing with the front cover removed, and a part of the configuration is simplified or omitted.
  • a bypass outlet 352 opens to the side surface of the thermal flow meter, and serves as a terminal end of the sub-passage.
  • FIG. 13 is an enlarged view of the right side view, and a part of the configuration is simplified or omitted.
  • the thickness (w1 + w2) of the measurement main body 310 of the thermal flow meter in the direction orthogonal to the insertion direction of the thermal flow meter at the dust discharge port position and the flow direction in the intake pipe is an opening at which the dust discharge port 355 opens into the main passage.
  • the plane includes the center of gravity P of the surface, and has different lengths (w1 ⁇ w2) on the basis of a plane perpendicular to the opening surface and parallel to the insertion direction of the thermal flow meter (center of gravity plane C). This is the same as in the first embodiment.
  • the opening position of the dust discharge port 355 is the same as that of the first embodiment, and the dust discharge port 35 is arranged at a position shifted with respect to the backflow direction of the backflow IC.
  • FIG. 14 is a schematic view of the EE cross section of FIG.
  • the main intake air flows forward from the upstream side to the downstream side as the gas to be measured IA, it flows from the upper side to the lower side as shown in FIG.
  • a pair of wake vortices IB are formed substantially symmetrically on the downstream side of the thermal flow meter. These wake vortices IB merge at an intermediate position therebetween to form a backflow IC directed toward the lower end surface of the measurement unit main body 310.
  • the air flow ID discharged from the dust discharge port 355 is generated toward the downstream side. Note that the cross-sectional area of the first passage (sub-passage) 31 toward the dust discharge port 355 is reduced by the inclined surface toward the dust discharge port 355, and the flow velocity of air passing through this portion is reduced. It is increasing.
  • the air flow ID does not face the backflow IC from the front, the airflow ID is not easily obstructed by the backflow IC, and it is possible to reduce the dust discharge effect and the deterioration of the measurement error of the mass flow rate.
  • the sub-passage structure in the present embodiment is similar to that of the fourth embodiment, but is substantially the same configuration except that the outer shape of the discharge passage and the thermal flow meter are different.
  • FIG. 15 is an enlarged view of the right side view, and a part of the configuration is simplified or omitted.
  • the thickness (w1 + w2) of the measurement main body 310 of the thermal flow meter in the direction orthogonal to the insertion direction of the thermal flow meter at the dust discharge port position and the flow direction in the intake pipe is an opening at which the dust discharge port 355 opens into the main passage.
  • the surface has a center of gravity P and has different lengths (w1 ⁇ w2) with reference to a plane (dotted line C) perpendicular to the opening surface and parallel to the insertion direction of the thermal flow meter. This is the same as in the first embodiment.
  • FIG. 16 is a schematic view of the FF cross section of FIG.
  • the shape of the passage toward the dust discharge port 355 includes a center of gravity P of the opening surface where the dust discharge port 355 opens into the main passage, and is a plane perpendicular to the opening surface and parallel to the insertion direction of the thermal flow meter (the center of gravity plane).
  • C) is symmetric with respect to the reference, but the external shape of the thermal flow meter is asymmetric. Since the outer shape is asymmetric, a pair of wake vortices IB generated on the downstream side of the thermal flow meter are also generated in an asymmetric shape.
  • the sub-passage structure in the present embodiment is similar to that in the fourth embodiment, but the configuration is substantially the same except that the discharge passage and the thermal flow meter are different.
  • FIG. 17 is an enlarged view of the right side view, and a part of the configuration is simplified or omitted.
  • the thickness (w1 + w2) of the measurement unit body 310 of the thermal flow meter in the direction orthogonal to the insertion direction of the thermal flow meter and the flow direction in the intake pipe at the maximum thickness position of the thermal flow meter is determined by the dust discharge port 355 being the main passage.
  • FIG. 18 is a schematic view of the GG cross section of FIG.
  • the shape of the passage toward the dust discharge port 355 includes a center of gravity P of the opening surface where the dust discharge port 355 opens into the main passage, and is a plane perpendicular to the opening surface and parallel to the insertion direction of the thermal flow meter (the center of gravity plane). It is asymmetric with respect to C), and the external shape of the thermal flow meter is also asymmetric. Since the outer shape is asymmetric, a pair of wake vortices IB generated on the downstream side of the thermal flow meter are also generated in an asymmetric shape.
  • the dust discharge port 355 is deflected to the back cover 304 side, but at the maximum thickness position (w1 + w2) of the thickness of the thermal flow meter, different lengths (w1) with respect to the center of gravity plane C. ⁇ w2).
  • these wake vortices IB merge at a position deviated from the plane (center of gravity plane C) to form a counterflow IC toward the thermal flow meter.
  • the air flow ID discharged from the dust discharge port 355 is generated toward the downstream side. Since the air flow ID does not face the reverse flow IC from the front, the discharge flow ID is not easily obstructed by the reverse flow IC, and it is possible to reduce the dust discharge effect and the deterioration of the measurement error of the mass flow rate.
  • the present invention is not limited to the above-described embodiments, and various designs can be made without departing from the spirit of the present invention described in the claims. It can be changed.
  • the above-described embodiment has been described in detail for easy understanding of the present invention, and is not necessarily limited to one having all the configurations described.
  • a part of the configuration of an embodiment can be replaced with the configuration of another embodiment, and the configuration of another embodiment can be added to the configuration of an embodiment.
  • DESCRIPTION OF SYMBOLS 30 ... Thermal flow meter, 31 ... 1st channel

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  • Physics & Mathematics (AREA)
  • Fluid Mechanics (AREA)
  • General Physics & Mathematics (AREA)
  • Measuring Volume Flow (AREA)
PCT/JP2016/080893 2015-10-28 2016-10-19 熱式流量計 WO2017073417A1 (ja)

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DE112016004950.1T DE112016004950T5 (de) 2015-10-28 2016-10-19 Thermischer durchflussmesser
US15/771,007 US10670439B2 (en) 2015-10-28 2016-10-19 Thermal flowmeter
CN201680058323.3A CN108139248B (zh) 2015-10-28 2016-10-19 热式流量计

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US11237035B2 (en) * 2017-12-27 2022-02-01 Hitachi Astemo, Ltd. Physical quantity detecting device
US11067419B2 (en) 2018-01-22 2021-07-20 Hitachi Automotive Systems, Ltd. Thermal flowmeter
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Family Cites Families (12)

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FR2776379B1 (fr) * 1998-03-19 2000-04-28 Schlumberger Ind Sa Compteur de gaz a filtres anti-poussieres
DE10246069A1 (de) * 2002-10-02 2004-04-15 Robert Bosch Gmbh Vorrichtung zur Bestimmung wenigstens eines Parameters eines in einer Leitung strömenden Mediums
JP3832498B1 (ja) * 2005-06-24 2006-10-11 オムロン株式会社 流量測定装置
JP5263324B2 (ja) 2011-03-24 2013-08-14 株式会社デンソー 空気流量測定装置
JP5408195B2 (ja) * 2011-07-19 2014-02-05 株式会社デンソー 空気流量測定装置
JP5675705B2 (ja) * 2012-06-15 2015-02-25 日立オートモティブシステムズ株式会社 熱式流量計
JP5755185B2 (ja) * 2012-06-15 2015-07-29 日立オートモティブシステムズ株式会社 熱式流量計
JP5758850B2 (ja) * 2012-06-15 2015-08-05 日立オートモティブシステムズ株式会社 熱式流量計
JP5464294B2 (ja) * 2013-07-04 2014-04-09 株式会社デンソー 空気流量測定装置
JP6118700B2 (ja) * 2013-09-30 2017-04-19 日立オートモティブシステムズ株式会社 熱式流量計
JP6114673B2 (ja) * 2013-09-30 2017-04-12 日立オートモティブシステムズ株式会社 熱式流量計
JP6114674B2 (ja) * 2013-09-30 2017-04-12 日立オートモティブシステムズ株式会社 熱式流量計

Patent Citations (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO2015045435A1 (ja) * 2013-09-30 2015-04-02 日立オートモティブシステムズ株式会社 熱式流量計

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US10670439B2 (en) 2020-06-02
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CN108139248B (zh) 2019-12-24
CN108139248A (zh) 2018-06-08
US20180313680A1 (en) 2018-11-01

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